A SIMPLIFIED ALGORITHM FOR THE IDENTIFICATION OF LONGITUDINAL DYNAMICS OF AN AIRCRAFT

Flight Dynamics, Stability and Control of a Flexible Airplane

Computational Aerodynamics Analysis of a Light Aircraft

Calculating Aerodynamic & Stability Characteristics For Small fixed-wing UAVs based on Digital DATCOM

AN ALGORITHM FOR CALCULATING THE AERODYNAMIC DERIVATIVES OF A SUPER-SONIC MISSILE

Development of a Comprehensive Tool for Calculating the Aeromechanics Characteristics of High-Speed Aircraft

Derivation of Optimal Guidance and Control Problem

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Computational Techniques for Calculation of Missile Aerodynamic Coefficients

Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM